Developing supersonic combustion models with efficiency, accuracy and practicality is
important foundation to deeply understand the complex combustion processes in scramjet …

Large eddy simulation is used to study the gas-particle two-phase transverse jet in
supersonic flow. In this paper, the Eulerian method is used to simulate the fluid, and the …

The annular scram combustor is a popular configuration for combined engines owing to its
compatibility with both turbines and rockets and its ability to withstand high flame …

In this study we use finite rate chemistry Large Eddy Simulation (LES) to examine flow,
injection, mixing, self-ignition and turbulent combustion in a dual-mode ramjet combustor …

Large Eddy Simulation (LES) has rapidly developed into a powerful computational
methodology for fluid dynamic studies, between Reynolds-Averaged Navier–Stokes (RANS) …

Characteristics of continuous rotating detonation (CRD) in a cavity-based annular combustor
are studied through three-dimensional simulations, which are solved in OpenFOAM with a …

The present study numerically investigates the combustion characteristics and performance
of a direct-connect gaseous hydrogen-fueled scramjet combustor depending on the injector …

The exploration of efficient combustion organization schemes is crucial as the expansion of
scramjet to higher Mach number becomes a cutting-edge trend. This paper evaluates the …

The annular scramjet combustor is considered one of the best configurations for a wide-
speed-range combined engine, owing to its superior thermal protection performance and …

Well-known analytical approaches are commonly adopted for the preliminary design of
scramjet engines. In this context, the combustion process in the combustion chamber can be …